WO2012084995A1 - Preform for blow moulding a container, mould part and elongate core for moulding the preform and method for stretch blow moulding the preform - Google Patents
Preform for blow moulding a container, mould part and elongate core for moulding the preform and method for stretch blow moulding the preform Download PDFInfo
- Publication number
- WO2012084995A1 WO2012084995A1 PCT/EP2011/073467 EP2011073467W WO2012084995A1 WO 2012084995 A1 WO2012084995 A1 WO 2012084995A1 EP 2011073467 W EP2011073467 W EP 2011073467W WO 2012084995 A1 WO2012084995 A1 WO 2012084995A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- preform
- preform according
- elongate
- body section
- moulding
- Prior art date
Links
- 238000000071 blow moulding Methods 0.000 title claims abstract description 33
- 238000000465 moulding Methods 0.000 title claims abstract description 32
- 238000000034 method Methods 0.000 title claims abstract description 16
- 238000002347 injection Methods 0.000 claims abstract description 16
- 239000007924 injection Substances 0.000 claims abstract description 16
- 239000012815 thermoplastic material Substances 0.000 claims abstract description 13
- 230000006835 compression Effects 0.000 claims abstract description 7
- 238000007906 compression Methods 0.000 claims abstract description 7
- 238000001125 extrusion Methods 0.000 claims abstract description 7
- 230000008719 thickening Effects 0.000 claims description 20
- 239000000203 mixture Substances 0.000 claims description 9
- 230000003247 decreasing effect Effects 0.000 claims description 6
- 230000001154 acute effect Effects 0.000 claims description 3
- 239000000463 material Substances 0.000 description 13
- 238000001746 injection moulding Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000009828 non-uniform distribution Methods 0.000 description 3
- 229920000139 polyethylene terephthalate Polymers 0.000 description 3
- 239000005020 polyethylene terephthalate Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 235000014171 carbonated beverage Nutrition 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- -1 polyethylene terephthalate Polymers 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/02—Combined blow-moulding and manufacture of the preform or the parison
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/02—Combined blow-moulding and manufacture of the preform or the parison
- B29C49/06—Injection blow-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/071—Preforms or parisons characterised by their configuration, e.g. geometry, dimensions or physical properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/4205—Handling means, e.g. transfer, loading or discharging means
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D1/00—Containers having bodies formed in one piece, e.g. by casting metallic material, by moulding plastics, by blowing vitreous material, by throwing ceramic material, by moulding pulped fibrous material, by deep-drawing operations performed on sheet material
- B65D1/02—Bottles or similar containers with necks or like restricted apertures, designed for pouring contents
- B65D1/0223—Bottles or similar containers with necks or like restricted apertures, designed for pouring contents characterised by shape
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/06—Making preforms by moulding the material
- B29B11/08—Injection moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/06—Making preforms by moulding the material
- B29B11/12—Compression moulding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/02—Combined blow-moulding and manufacture of the preform or the parison
- B29C2049/023—Combined blow-moulding and manufacture of the preform or the parison using inherent heat of the preform, i.e. 1 step blow moulding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/0715—Preforms or parisons characterised by their configuration the preform having one end closed
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/072—Preforms or parisons characterised by their configuration having variable wall thickness
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/073—Preforms or parisons characterised by their configuration having variable diameter
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/074—Preforms or parisons characterised by their configuration having ribs or protrusions
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/076—Preforms or parisons characterised by their configuration characterised by the shape
- B29C2949/0761—Preforms or parisons characterised by their configuration characterised by the shape characterised by overall the shape
- B29C2949/0763—Axially asymmetrical
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/076—Preforms or parisons characterised by their configuration characterised by the shape
- B29C2949/0768—Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform
- B29C2949/077—Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform characterised by the neck
- B29C2949/0772—Closure retaining means
- B29C2949/0773—Threads
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/076—Preforms or parisons characterised by their configuration characterised by the shape
- B29C2949/0768—Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform
- B29C2949/0779—Preforms or parisons characterised by their configuration characterised by the shape characterised by the shape of specific parts of preform characterised by the body
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/079—Auxiliary parts or inserts
- B29C2949/0795—Parts to assist orientation of preform, e.g. in mould
- B29C2949/0798—Parts to assist orientation of preform, e.g. in mould at body portion
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/079—Auxiliary parts or inserts
- B29C2949/08—Preforms made of several individual parts, e.g. by welding or gluing parts together
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/081—Specified dimensions, e.g. values or ranges
- B29C2949/0811—Wall thickness
- B29C2949/0817—Wall thickness of the body
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/081—Specified dimensions, e.g. values or ranges
- B29C2949/0839—Angle
- B29C2949/0845—Angle of the body
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/20—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
- B29C2949/22—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at neck portion
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/20—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
- B29C2949/24—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at flange portion
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/20—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
- B29C2949/26—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at body portion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/20—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
- B29C2949/28—Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at bottom portion
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3024—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3032—Preforms or parisons made of several components having components being injected
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3056—Preforms or parisons made of several components having components being compression moulded
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/76—Cores
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2067/00—Use of polyesters or derivatives thereof, as moulding material
- B29K2067/003—PET, i.e. poylethylene terephthalate
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/1397—Single layer [continuous layer]
Definitions
- the present invention relates to a preform, in particular an elongate preform for blow moulding into a container such as a bottle.
- blow moulding is often used in the manufacture of containers, particularly bottles, for example for carbonated beverages.
- This process involves the initial formation of a preform, typically by injection moulding, which preforms are subsequently blow moulded to form the containers.
- preforms are typically formed of thermoplastic material, particularly polyethylene terephthalate (PET).
- the preform is blow moulded from its original shape, i.e. the shape imparted to it during the injection moulding process.
- Conventional blow-moulding involves the step of heating the preform prior to inserting the heated preform into a blow moulding machine. In the blow moulding machine, air is blown into the preform to stretch the preform outwardly so that the container thereby formed assumes a shape defined by a hollow blow moulding cavity.
- Some blow moulded containers require shapes which are not rotationally symmetrical, for example the cross-section of a bottle may be oval rather than circular.
- a preform which has a non-uniform distribution of material around its circumference which reflects the non-uniform shape of the intended blow-moulded container.
- regions of the preform which are to be highly stretched, causing a high degree of thinning of the sidewall thickness during blow moulding are provided with an initial higher wall thickness as compared to regions which are to be less stretched.
- the conventional process for producing a preform is an injection moulding process.
- the elongate preform is injection moulded around an elongate core, which may be water cooled, which has external shape and dimensions which define the internal surface of the preform.
- the core comprises a male mould element having a convex moulding surface.
- the external surface of the preform is moulded by a complementary female mould element constituted by a mould block, which may comprise two mating mould halves, having an elongate cavity which defines an elongate concave moulding surface.
- the mould block conventionally has a cavity which has a surface of rotation around a central longitudinal axis, and thus the external elongate longitudinally extending surface of the preform has a surface of rotation around a central longitudinal axis.
- the core has a non-uniform surface which does not have surface of rotation around a central longitudinal axis and thus the internal elongate longitudinally extending surface of the preform has a non-uniform surface which is not a surface of rotation around a central longitudinal axis.
- the preform after the preform has been injection moulded from a liquid plastic material solidifying within the mould, it is necessary to remove the preform from the mould.
- This requires the elongate core preform carrying the solid moulded preform moulded therearound to be remove from the mould block cavity, and then for the solid moulded preform to be longitudinally stripped off the elongate core.
- the core In order to ensure that the preform can be easily pulled off the core, and not become stuck on the core, the core progressively decreases in diameter in a longitudinal direction from a fixed end of the core, which is mounted to a support and moulds the open neck of the preform, and a free end of the core which moulds the base-forming portion of the preform.
- the longitudinal surface of the core along any given longitudinal line has a shallow draft angle, of up to a few degrees, to provide such a diameter decrease. Accordingly, along any given longitudinal line on the core surface extending from the free end to the fixed end, the surface progressively does not decrease in distance from a longitudinal centre line of the core. This ensures that the internal surface of the preform correspondingly, progressing along any given longitudinal line on the internal surface extending from the closed base- forming end to the open neck, does not decrease in distance from a longitudinal centre line of the preform.
- the internal cavity of the preform, and the external surface of the core which moulds that internal cavity only progressively increase in a direction from the closed end of the preform to the open end of the preform.
- the present invention aims to at least partially to overcome these problems of known preforms for blow moulding containers having a rotationally non-uniform shape, i.e. the containers do not have a sidewall which is a surface of rotation.
- a preform structure which can improve the material distribution in such stretch blow-moulded containers.
- the present invention provides a preform for blow moulding to form a container, the preform being formed of a thermoplastic material, the preform comprising a neck finish at an open end of the preform, an elongate body section and a closed end, wherein the body section has elongate, longitudinally extending inner and outer surfaces each centered about a longitudinal axis of the preform, the inner and outer surfaces defining therebetween a wall of the body section, wherein the wall of the body section has at least one locally thickened portion along the body section, the locally thickened portion being thicker than adjacent first and second thinner portions at respective opposite longitudinal ends of the thickened portion, the thickened portion having an inner surface portion which is nearer to the longitudinal axis than respective first and second inner surface portions of the first and second thinner portions.
- the wall thickness changes between the locally thickened portion and the adjacent first and second thinner portions are smoothly continuously inclined in the longitudinal direction.
- the preform comprises first and second inclined inner faces, each at a respective first and second blend angle, relative to the longitudinal axis, for the respective first and second inner surface portions extending away from the locally thickened portion.
- first and second inclined inner faces are respectively oriented towards the open end and the closed end, and the first blend angle is smaller than the second blend angle.
- the locally thickened portion defines a ridge on the inner surface.
- the ridge is linear and extends orthogonally to the longitudinal axis. Still further optionally, the ridge extends along an angular segment of less than 90° of the inner surface.
- At least one of the first and second thinner portions comprises a part of a longitudinally extending thickened element which, along its length, is thicker than laterally adjacent regions of the wall on respective opposite lateral sides of the element.
- the element comprises a radially inwardly directed angular segment.
- at least a part of the longitudinally extending thickened element has a planar chordal inner surface.
- the preform comprises two locally thickened portions, each provided at a respective one of two longitudinally spaced locations along the body section. Further optionally, a first locally thickened portion is located at a lowermost third of the length of the body section adjacent to the closed end and a second locally thickened portion is located at an uppermost third of the length of the body section adjacent to the open end.
- the body section is longitudinally symmetrical and has a plurality of locally thickened portions annularly disposed around the preform.
- the elongate, longitudinally extending inner surface has an n-fold longitudinal axis of symmetry, where n is at least 2. Typically, n is 2, 3, 4, 5 or 6, or any larger number.
- the body section has a plurality of locally thickened portions alternating around the circumference of the preform with portions of constant thickness.
- the portions of constant thickness extend for substantially the entire length of the body section.
- the portions of constant thickness have outer and inner surfaces which extend substantially parallel to the longitudinal axis, optionally with a draft angle of less than 1 ° extending from the closed end to the open end.
- a thickening compared to laterally adjacent regions on respective opposite lateral sides of the thickening, the thickening comprising a first ramp section of increasing wall thickness, a second ramp section of decreasing wall thickness, an elongate constant thickness section, a third ramp section of increasing wall thickness and a fourth ramp section of decreasing wall thickness.
- the first and second ramp sections define a first transverse ridge therebetween which is closer to the longitudinal axis than the first and second ramp sections.
- the third and fourth ramp sections define a second transverse ridge therebetween which is closer to the longitudinal axis than the third and fourth ramp sections.
- the elongate constant thickness section has opposed linear longitudinally extending edges.
- a respective thickening is provided along each of two opposed angular segments of the body section.
- the elongate, longitudinally extending outer surface has a circular cross- section.
- the elongate, longitudinally extending outer surface is substantially right cylindrical, optionally with a draft angle of less than ⁇ extending from the closed end to the open end.
- the present invention further provides a mould part for forming a preform according to the present invention, the mould part comprising a central elongate core having an outer surface corresponding to the inner surface of the preform.
- the mould part may be adapted for use in an injection mould or an extrusion compression mould.
- the present invention further provides an elongate core of an injection mould or an extrusion compression mould for forming a moulded preform of a thermoplastic material for stretch blow moulding to form a container, the core comprising a fixed end, an elongate body and a free end, the elongate body defining a convex elongate, longitudinally extending moulding surface for moulding an internal surface of a body section of the preform, the first moulding surface having a cross-section centered about a longitudinal axis, and being substantially cylindrical with an acute draft angle to provide that the free end has a smaller diameter than that of the fixed end, the moulding surface including at least one concave undercut where the core is machined below the draft angle of the core.
- the core may be a movable core as disclosed, for example, in the present inventor's earlier WO-A-2008/084230 and WOA-2009/044142.
- the present invention further provides a method for blow moulding a preform according to the present invention to form a container having a non-circular cross-section including first opposed faces separated by a major internal dimension and second opposed faces separated by a minor internal dimension, said method including the step of:
- the present invention is predicated on the finding by the present inventor that by providing the preform inner surface with one or more regions which are located inwardly towards the central longitudinal axis of the preform that adjacent regions which are nearer to the closed base-forming end of the preform, the minimum additional thermoplastic material can be employed to strengthen particular regions of the bottle blown from the preform. This leads to strengthened bottles, particularly non-circular bottles such as oval or rectangular cross-section bottles, which yet have minimum weight, with consequential material and cost savings.
- Such an inner surface structure for the preform is achieved by sculpturing the elongate core on which the preform is moulded from liquid thermoplastic material, the core defining the cavity within the preform and the outer surface of the core corresponding to the inner surface of the preform.
- the sculpturing of the outer surface of the core includes undercutting the core surface, so as to provide a concave undercut where the core is machined below the draft angle of the core. Undercutting the core would be regarded by the person skilled in the art as illogical if one assumes that the preform is cold, and so the thermoplastic material is substantially rigid, when the preform is stripped off the core, since in such a condition the undercuts would cause very high stripping loads, therefore causing high stress in the preform, which is undesirable.
- thermoplastic material of the preform is in a pliable state when stripping occurs, and therefore the preform structure, and in particular the inner surface, can easily accommodate deep undercuts as long as there are gentle ramps to accommodate the undercut depth.
- Such a concave undercut causes the moulded preform have a corresponding convexity in the inner surface.
- the stripping action may deform the convexity so as to tend to flatten it, but the convexity tends also to expand back to the previously moulded configuration when stripped off the core, so as to "bump out" of the undercut.
- Undercuts can be applied in areas of the core that relate to the bottom corners of an oval bottle to reduce the problem of over- thinning when the bottle is stretch blown from the preform.
- the undercut can be applied as a continuous band around the core to create stiffening in an area of transition from a circular or round cross-section to an oval cross-section.
- Oval bottles that have a small corner radius and/or a small top shoulder radius benefit from side undercuts near the top and bottom of the core to reinforce these normally thin areas. It is also possible to add undercuts wherever bottle thinning take place, effectively sculpturing the core to minimise preform weight.
- Round bottles with a small bottom corner radius benefit from a continuous undercut band near the bottom of the core that is positioned so as to align with the radius to ensure corner strength when stretch blown.
- the development work by the present inventor has shown that locally thickening the preform, related to the final position in the bottle, has allowed the achievement of a substantially reduced weight in oval bottles. Undercutting the core creates sufficient local thickening of structural regions of the bottle which are particularly susceptible to weakness due to localized thinning, without over-weighting the bottle.
- Figure 1 is a schematic cross-sectional side view, from a first direction, of a preform in accordance with a first embodiment of the present invention, and also showing a front shape of a bottle to be blow-moulded from the preform;
- Figure 2 is a schematic cross-sectional side view, from a second direction, of the preform of Figure 1, and also showing a side shape of the bottle shown in Figure 1 ;
- Figure 3 is a schematic cross-section on line A-A through the preform of Figure 1 ;
- Figure 4 is a schematic cross-section on line B-B through the preform of Figure 1 ;
- Figure 5 is a schematic cross-section on lines C-C and D-D through the preform of Figure 1.
- the preform 2 for blow moulding a container 3 such as a bottle, in accordance with an embodiment of the present invention, the preform having been formed by an injection moulding process.
- the preform 2 comprises a thermoplastic material, such as PET.
- the elongate preform 2 has a conventional hollow structure and comprises a neck finish 4, which may be threaded, including an annular closure seating flange 6, at an open end 8 of the preform 2, a main body section 10 and a closed end 12 having a convex outer surface 14, and a corresponding concave inner surface 16, which are typically substantially hemispherical.
- the main body section 10 is substantially cylindrical.
- the main body section 10 has an elongate, longitudinally extending inner surface 18 and an elongate, longitudinally extending outer surface 20.
- the outer surface 20 has a circular cross-section, and typically is substantially right cylindrical.
- the inner surface 18 has a small taper, of a draft angle typically less than , along the entire length or at least towards the closed end 12 to enable the injection moulded preform 2 readily to be removed from the core of the injection mould.
- the outer surface 20 has a small taper, of a draft angle typically less than , along the entire length or at least towards the closed end 12 to enable the injection moulded preform readily to be removed from the moulding block of the injection mould.
- the inner surface 18 and outer surface 20 are each centered about a longitudinal axis L-L of the preform 2.
- the inner and outer surfaces 18, 20 define therebetween a wall 22 of the body section 10.
- the wall 22 of the body section 10 has at least one locally thickened portion 24, 26 along the body section 10.
- Each locally thickened portion 24, 26 is thicker than adjacent first and second thinner portions 28, 30; 32, 34 located at respective opposite longitudinal ends of the thickened portion 24, 26.
- the thickened portion 24, 26 has an inner surface portion 36, 38 which is nearer to the longitudinal axis L-L than respective first and second inner surface portions 40, 42; 44, 46 of the first and second thinner portions 28, 30; 32, 34.
- the wall thickness changes between the locally thickened portion 24, 26 and the adjacent first and second thinner portions 28, 30; 32, 34 are smoothly continuously inclined in the longitudinal direction.
- the preform 2 comprises first and second inclined inner faces 48, 50; 52, 54, each at a respective first and second blend angle ⁇ , ⁇ , relative to the longitudinal axis L-L, for the respective first and second inner surface portions 40, 42; 44, 46 extending away from the locally thickened portion 24, 26.
- the first and second inclined inner faces 48, 50; 52, 54, are respectively oriented towards the open end 8 and the closed end 12, and the first blend angle a is smaller than the second blend angle ⁇ .
- the locally thickened portion 24, 26 defines a ridge 56, 58 on the inner surface 18.
- the ridge 56, 58 is linear and extends orthogonally to the longitudinal axis L-L, and along an angular segment 60 of less than 90° of the inner surface 18.
- the first and second thinner portions 32, 30 comprises a part of a longitudinally extending thickened element 62 which, along its length, is thicker than laterally adjacent regions 64, 66 of the wall 22 on respective opposite lateral sides of the element 62.
- the element 62 comprises a radially inwardly directed angular segment. At least a part of the element 62 has a planar chordal inner surface 68.
- the preform 2 comprises two locally thickened portions 24, 26, each provided at a respective one of two longitudinally spaced locations along the body section 10.
- a first locally thickened portion 24 is located at a lowermost third of the length of the body section 10 adjacent to the closed end 12 and a second locally thickened portion 26 is located at an uppermost third of the length of the body section 10 adjacent to the open end 8.
- the body section 10 is longitudinally symmetrical and has a plurality of locally thickened portions 24, 26 annularly disposed around the preform 2.
- the inner surface 18 has an n-fold longitudinal axis of symmetry, where n is at least 2, typically 2 as in the illustrated embodiment, for example 2, 3, 4, 5 or 6, or any larger number.
- the body section 10 has a plurality of locally thickened portions 24, 26 alternating around the circumference of the preform 2 with wall portions 70 of constant thickness.
- the portions 70 of constant thickness extend for substantially the entire length of the body section 10.
- the portions 70 of constant thickness have outer and inner surfaces 18, 20 which extend substantially parallel to the longitudinal axis, optionally with a draft angle of less than 1 ° extending from the closed end 12 to the open end 8.
- the thickening comprises a first ramp section of increasing wall thickness, for example formed of first thinner portion 28; a second ramp section of decreasing wall thickness, for example formed of second thinner portion 30; an elongate constant thickness section, for example formed of longitudinally extending thickened element 62; a third ramp section of increasing wall thickness, for example formed of first thinner portion 32; and a fourth ramp section of decreasing wall thickness, for example formed of second thinner portion 30.
- the first and second ramp sections 28, 30 define a first transverse ridge 56 therebetween which is closer to the longitudinal axis than the first and second ramp sections 28, 30.
- the third and fourth ramp sections 32, 34 define a second transverse ridge 58 therebetween which is closer to the longitudinal axis than the third and fourth ramp sections 32, 34.
- the elongate constant thickness section 62 has opposed linear longitudinally extending edges 74, 76. As shown in the illustrated embodiment, a respective thickening 72 is provided along each of two opposed angular segments of the body section.
- the wall thickness changes provided by the ramp sections are smooth so as to avoid any stress concentrations in the preform 2 or the resultant blow moulded container 3.
- Figure 3 is a schematic cross-section on line A-A through the preform 2, and in the illustrated embodiment the constant wall thickness x at that point (Point D) is 2.0 mm.
- Figure 4 is a schematic cross-section on line B-B through the preform 2, and in the illustrated embodiment the opposed elongate constant thickness sections 62 have a maximum wall thickness y of 2.5 mm, alternating with the constant wall thickness x of 2.0 mm, this structure being at Point D.
- Figure 5 is a schematic cross-section on lines C- C and D-D through the preform 2, and in the illustrated embodiment the opposed ridges 56. 58 have a maximum wall thickness z of 3.0 mm, alternating with the constant wall thickness x of 2.0 mm, this structure being at Points A and C.
- the thickening 72 typically extends for substantially the entire length, parallel to axis L- L, of the main body section 10. However, depending upon the shape and configuration of the desired blow moulded container to be made from the preform 2, the thickening 72 may alternatively extend for only a proportion, even a minor proportion (i.e. less than 50%), of the length of the main body section 10.
- the n-fold axis of symmetry for the thickenings 72 may have a different value, for example 3 for making a container having a substantially triangular cross-section, or 8 or greater for making a multi-faceted container.
- the preform illustrated in Figures 1 to 5 is heated and inserted into a stretch blow moulding apparatus, and is stretch blow moulded from the substantially tubular shape to the shape desired for the final container 3
- the present invention has particular application in a method for blow moulding a preform 2 to form a container 3 having a non-circular cross-section including first opposed faces 80, 82 separated by a major internal dimension and second opposed faces 84, 86 separated by a minor internal dimension
- the preform 2 is rotationally oriented in a blow moulding apparatus so that the at least one locally thickened portion 24, 26, or the thickening 72, is oriented towards a moulding surface for moulding such a first opposed face 80, 82.
- Points A, B, C and D indicated for the preform 2 correlate to Points A, B, C and D indicated for the container 3 stretch blow-moulded therefrom.
- each lower ridge 56 substantially forms a respective bottom corner 88 of the container 3 which is located between the container base 90 and the respective first opposed faces 80, 82.
- the stretch ratio of the thermoplastic material forming that bottom corner 88 is higher than for any other portion of the container 3, and so the thickened preform material at the ridge 56 prevents over-thinning at that corner 88.
- each upper ridge 58 substantially forms a respective upper corner 92 of the container 3 which is located between the container shoulder 94 and the respective first opposed faces 80, 82.
- the first opposed faces 80, 82 are substantially formed from the central portion of the thickening 72 between the ridges 56, 58, in particular the second ramp section formed of second thinner portion 30; the elongate constant thickness section formed of longitudinally extending thickened element 62; and the third ramp section formed of first thinner portion 32.
- the relatively thickened wall portions of the preform 2 may be preferentially stretched, by having a higher radial stretch ratio, as compared to the relatively thinned wall portions, to provide a substantially uniform sidewall thickness in the resultant non- circular container 3. Even in highly stretched regions of the sidewall, the desired minimum wall thickness has been maintained because these regions are formed from the relatively thickened wall portions of the preform 2.
- the shaping of the preform according to the invention may be regarded as an "ovalisation" of the preform where there are vertical areas on the inner surface that are thickened to help maintain wall thickness in the highly stretched areas of the bottle.
- These thickened areas may be considered to constitute a plurality of integral longitudinal thickened ribs disposed in a mutually spaced configuration around the circular inner surface.
- Such an "ovalisation” structure is achieved by undercutting the core, which minimizes excess material while providing additional material precisely where it is required in the container and particularly at highly stretched corners of container faces remote from the longitudinal axis.
- the invention also provides an injection mould or an extrusion compression mould for forming a preform according to the present invention.
- the injection mould comprises a central elongate core and a mould block defining a cavity for receiving the core.
- the central elongate core has an outer surface corresponding to the inner surface of the preform.
- the core includes a convex elongate, longitudinally extending first moulding surface for moulding an internal surface of a body section of the preform, the first moulding surface having a cross-section centered about a longitudinal axis.
- the cavity includes a concave elongate, longitudinally extending second moulding surface for moulding an external surface of the body section of the preform, the second moulding surface having a circular cross-section centered about the longitudinal axis.
- the elongate core may be of an injection mould or an extrusion compression mould for forming a moulded preform of a thermoplastic material for stretch blow moulding to form a container.
- the core comprises a fixed end, an elongate body and free end, the elongate body defining a convex elongate, longitudinally extending moulding surface for moulding an internal surface of a body section of the preform, the first moulding surface having a cross-section centered about a longitudinal axis, and being substantially cylindrical with an acute draft angle to provide that the free end has a smaller diameter than that of the fixed end, the moulding surface including at least one concave undercut where the core is machined below the draft angle of the core
- the present invention also provides a method for blow moulding a preform according to the present invention, to form a container.
- the container has a non-circular cross-section including first opposed faces separated by a major internal dimension and second opposed faces separated by a minor internal dimension.
- the method includes the step of rotationally orienting the preform in a blow moulding apparatus so that the at least one locally thickened portion is oriented towards moulding surface for moulding a first opposed face.
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Abstract
A preform (2) for blow moulding to form a container (3), the preform being formed of a thermoplastic material, the preform comprising a neck finish (4) at an open end (8) of the preform, an elongate body section (10) and a closed end (12), wherein the body section has elongate, longitudinally extending inner (18) and outer surfaces (20) each centered about a longitudinal axis of the preform, the inner and outer surfaces defining therebetween a wall of the body section, wherein the wall of the body section has at least one locally thickened portion (24, 26) along the body section, the locally thickened portion being thicker than adjacent first and second thinner portions (28, 30; 32, 24) at respective opposite longitudinal ends of the thickened portion, the thickened portion having an inner surface portion (36, 38) which is nearer to the longitudinal axis than respective first and second inner surface portions of the first and second thinner portions. A mould part and an elongate core of an injection mould or an extrusion compression mould for moulding the preform, and a method for stretch blow moulding the preform is also disclosed.
Description
PREFORM FOR BLOW MOULDING A CONTAINER, MOULD PART AND ELONGATE CORE FOR MOULDING THE PREFORM AND METHOD FOR STRETCH BLOW MOULDING THE PREFORM
The present invention relates to a preform, in particular an elongate preform for blow moulding into a container such as a bottle.
In the packaging industry, the process of blow moulding is often used in the manufacture of containers, particularly bottles, for example for carbonated beverages. This process involves the initial formation of a preform, typically by injection moulding, which preforms are subsequently blow moulded to form the containers. Such preforms are typically formed of thermoplastic material, particularly polyethylene terephthalate (PET).
In the conventional blow-moulding process, the preform is blow moulded from its original shape, i.e. the shape imparted to it during the injection moulding process. Conventional blow-moulding involves the step of heating the preform prior to inserting the heated preform into a blow moulding machine. In the blow moulding machine, air is blown into the preform to stretch the preform outwardly so that the container thereby formed assumes a shape defined by a hollow blow moulding cavity.
Some blow moulded containers require shapes which are not rotationally symmetrical, for example the cross-section of a bottle may be oval rather than circular. In order to attempt to maintain uniform material properties, for example biaxial orientation, and uniform sidewall thickness, it is known to provide a preform which has a non-uniform distribution of material around its circumference which reflects the non-uniform shape of the intended blow-moulded container. For example, regions of the preform which are to be highly stretched, causing a high degree of thinning of the sidewall thickness during blow moulding, are provided with an initial higher wall thickness as compared to regions which are to be less stretched.
The conventional process for producing a preform is an injection moulding process. The elongate preform is injection moulded around an elongate core, which may be water cooled, which has external shape and dimensions which define the internal surface of the preform. The core comprises a male mould element having a convex moulding surface.
The external surface of the preform is moulded by a complementary female mould element constituted by a mould block, which may comprise two mating mould halves, having an elongate cavity which defines an elongate concave moulding surface.
When a preform which has a non-uniform distribution of material around its circumference is required to be manufactured, it is conventional to machine the convex surface of the male mould element to have a rotationally non-uniform surface. The result is that the internal surface of the elongate preform, which is moulded by the core, has a rotationally non-uniform surface. This is because machining an elongate convex surface to introduce such non-uniformity is technically simpler and less costly than machining an elongate concave surface. The less expensive core of the injection moulding machine can readily be swapped for another of different dimensions or shape depending on the structure of the selected preform to be injection moulded, while retaining a common more expensive mould block.
The mould block conventionally has a cavity which has a surface of rotation around a central longitudinal axis, and thus the external elongate longitudinally extending surface of the preform has a surface of rotation around a central longitudinal axis. When a preform which has a non-uniform distribution of material around its circumference is manufactured, the core has a non-uniform surface which does not have surface of rotation around a central longitudinal axis and thus the internal elongate longitudinally extending surface of the preform has a non-uniform surface which is not a surface of rotation around a central longitudinal axis.
However, after the preform has been injection moulded from a liquid plastic material solidifying within the mould, it is necessary to remove the preform from the mould. This requires the elongate core preform carrying the solid moulded preform moulded therearound to be remove from the mould block cavity, and then for the solid moulded preform to be longitudinally stripped off the elongate core. In order to ensure that the preform can be easily pulled off the core, and not become stuck on the core, the core progressively decreases in diameter in a longitudinal direction from a fixed end of the core, which is mounted to a support and moulds the open neck of the preform, and a free
end of the core which moulds the base-forming portion of the preform. The longitudinal surface of the core along any given longitudinal line has a shallow draft angle, of up to a few degrees, to provide such a diameter decrease. Accordingly, along any given longitudinal line on the core surface extending from the free end to the fixed end, the surface progressively does not decrease in distance from a longitudinal centre line of the core. This ensures that the internal surface of the preform correspondingly, progressing along any given longitudinal line on the internal surface extending from the closed base- forming end to the open neck, does not decrease in distance from a longitudinal centre line of the preform. The internal cavity of the preform, and the external surface of the core which moulds that internal cavity, only progressively increase in a direction from the closed end of the preform to the open end of the preform.
There are a number of disadvantages to the provision of such a conventional structure for a preform for use in a subsequent blow moulding process, most particularly for blow moulding a non-circular container from a rotationally non-uniform preform. In particular, with such a structure it can be difficult to accurately control the material distribution within the blow-moulded container, or the stretch ratio in the various regions of the container having dimensional anisotropy, since the container has a shape which is not a surface of rotation. Some regions may be excessively stretched, leading to undesired high stretch ratios and excessive wall thinning. Furthermore, this can lead to corners of the container, such as a bottle, having undesired thickness, or even undesired thinness. Also, it is generally necessary to provide excess plastic material in the preform to ensure that at least the thinner preform regions are blow moulded into the desired container portions. This increases perform weight, and therefore container weight, and material cost.
The present invention aims to at least partially to overcome these problems of known preforms for blow moulding containers having a rotationally non-uniform shape, i.e. the containers do not have a sidewall which is a surface of rotation. There is therefore currently a need in the art for a preform structure which can improve the material distribution in such stretch blow-moulded containers.
The present invention provides a preform for blow moulding to form a container, the preform being formed of a thermoplastic material, the preform comprising a neck finish at an open end of the preform, an elongate body section and a closed end, wherein the body section has elongate, longitudinally extending inner and outer surfaces each centered about a longitudinal axis of the preform, the inner and outer surfaces defining therebetween a wall of the body section, wherein the wall of the body section has at least one locally thickened portion along the body section, the locally thickened portion being thicker than adjacent first and second thinner portions at respective opposite longitudinal ends of the thickened portion, the thickened portion having an inner surface portion which is nearer to the longitudinal axis than respective first and second inner surface portions of the first and second thinner portions.
Optionally, the wall thickness changes between the locally thickened portion and the adjacent first and second thinner portions are smoothly continuously inclined in the longitudinal direction.
Optionally, the preform comprises first and second inclined inner faces, each at a respective first and second blend angle, relative to the longitudinal axis, for the respective first and second inner surface portions extending away from the locally thickened portion. Further optionally, the first and second inclined inner faces are respectively oriented towards the open end and the closed end, and the first blend angle is smaller than the second blend angle.
Optionally, the locally thickened portion defines a ridge on the inner surface. Further optionally, the ridge is linear and extends orthogonally to the longitudinal axis. Still further optionally, the ridge extends along an angular segment of less than 90° of the inner surface.
Optionally, at least one of the first and second thinner portions comprises a part of a longitudinally extending thickened element which, along its length, is thicker than laterally adjacent regions of the wall on respective opposite lateral sides of the element. Further optionally, the element comprises a radially inwardly directed angular segment.
Optionally, at least a part of the longitudinally extending thickened element has a planar chordal inner surface.
Optionally, the preform comprises two locally thickened portions, each provided at a respective one of two longitudinally spaced locations along the body section. Further optionally, a first locally thickened portion is located at a lowermost third of the length of the body section adjacent to the closed end and a second locally thickened portion is located at an uppermost third of the length of the body section adjacent to the open end.
Optionally, the body section is longitudinally symmetrical and has a plurality of locally thickened portions annularly disposed around the preform.
Optionally, the elongate, longitudinally extending inner surface has an n-fold longitudinal axis of symmetry, where n is at least 2. Typically, n is 2, 3, 4, 5 or 6, or any larger number.
Optionally, the body section has a plurality of locally thickened portions alternating around the circumference of the preform with portions of constant thickness. Further optionally, the portions of constant thickness extend for substantially the entire length of the body section. Yet further optionally, the portions of constant thickness have outer and inner surfaces which extend substantially parallel to the longitudinal axis, optionally with a draft angle of less than 1 ° extending from the closed end to the open end.
Optionally, along at least one angular segment of the body section there is provided, in a direction from the open end to the closed end, a thickening compared to laterally adjacent regions on respective opposite lateral sides of the thickening, the thickening comprising a first ramp section of increasing wall thickness, a second ramp section of decreasing wall thickness, an elongate constant thickness section, a third ramp section of increasing wall thickness and a fourth ramp section of decreasing wall thickness.
Optionally, the first and second ramp sections define a first transverse ridge therebetween which is closer to the longitudinal axis than the first and second ramp sections.
Optionally, the third and fourth ramp sections define a second transverse ridge therebetween which is closer to the longitudinal axis than the third and fourth ramp sections.
Optionally, the elongate constant thickness section has opposed linear longitudinally extending edges.
Optionally, a respective thickening is provided along each of two opposed angular segments of the body section.
Optionally, the elongate, longitudinally extending outer surface has a circular cross- section.
Optionally, the elongate, longitudinally extending outer surface is substantially right cylindrical, optionally with a draft angle of less than Γ extending from the closed end to the open end.
The present invention further provides a mould part for forming a preform according to the present invention, the mould part comprising a central elongate core having an outer surface corresponding to the inner surface of the preform.
The mould part may be adapted for use in an injection mould or an extrusion compression mould.
The present invention further provides an elongate core of an injection mould or an extrusion compression mould for forming a moulded preform of a thermoplastic material for stretch blow moulding to form a container, the core comprising a fixed end, an elongate body and a free end, the elongate body defining a convex elongate,
longitudinally extending moulding surface for moulding an internal surface of a body section of the preform, the first moulding surface having a cross-section centered about a longitudinal axis, and being substantially cylindrical with an acute draft angle to provide that the free end has a smaller diameter than that of the fixed end, the moulding surface including at least one concave undercut where the core is machined below the draft angle of the core.
The core may be a movable core as disclosed, for example, in the present inventor's earlier WO-A-2008/084230 and WOA-2009/044142.
The present invention further provides a method for blow moulding a preform according to the present invention to form a container having a non-circular cross-section including first opposed faces separated by a major internal dimension and second opposed faces separated by a minor internal dimension, said method including the step of:
a. rotationally orienting the preform in a blow moulding apparatus so that the at least one locally thickened portion is oriented towards moulding surface for moulding a first opposed face.
The present invention is predicated on the finding by the present inventor that by providing the preform inner surface with one or more regions which are located inwardly towards the central longitudinal axis of the preform that adjacent regions which are nearer to the closed base-forming end of the preform, the minimum additional thermoplastic material can be employed to strengthen particular regions of the bottle blown from the preform. This leads to strengthened bottles, particularly non-circular bottles such as oval or rectangular cross-section bottles, which yet have minimum weight, with consequential material and cost savings.
Such an inner surface structure for the preform is achieved by sculpturing the elongate core on which the preform is moulded from liquid thermoplastic material, the core defining the cavity within the preform and the outer surface of the core corresponding to the inner surface of the preform. The sculpturing of the outer surface of the core includes undercutting the core surface, so as to provide a concave undercut where the core is machined below the draft angle of the core.
Undercutting the core would be regarded by the person skilled in the art as illogical if one assumes that the preform is cold, and so the thermoplastic material is substantially rigid, when the preform is stripped off the core, since in such a condition the undercuts would cause very high stripping loads, therefore causing high stress in the preform, which is undesirable.
However, the present inventor has found that in practice, a high percentage of the preform cooling is achieved after stripping of the preform from the core, for example when the preform is held in a take-out robot. This means that the thermoplastic material of the preform is in a pliable state when stripping occurs, and therefore the preform structure, and in particular the inner surface, can easily accommodate deep undercuts as long as there are gentle ramps to accommodate the undercut depth.
Such a concave undercut causes the moulded preform have a corresponding convexity in the inner surface. The stripping action may deform the convexity so as to tend to flatten it, but the convexity tends also to expand back to the previously moulded configuration when stripped off the core, so as to "bump out" of the undercut.
This means that the convexity formed during the moulding process is present in the final solidified preform, without excess stress being present in the preform.
Undercuts can be applied in areas of the core that relate to the bottom corners of an oval bottle to reduce the problem of over- thinning when the bottle is stretch blown from the preform. Alternatively, the undercut can be applied as a continuous band around the core to create stiffening in an area of transition from a circular or round cross-section to an oval cross-section.
Oval bottles that have a small corner radius and/or a small top shoulder radius benefit from side undercuts near the top and bottom of the core to reinforce these normally thin areas. It is also possible to add undercuts wherever bottle thinning take place, effectively sculpturing the core to minimise preform weight.
Round bottles with a small bottom corner radius benefit from a continuous undercut band near the bottom of the core that is positioned so as to align with the radius to ensure corner strength when stretch blown.
The development work by the present inventor has shown that locally thickening the preform, related to the final position in the bottle, has allowed the achievement of a substantially reduced weight in oval bottles. Undercutting the core creates sufficient local thickening of structural regions of the bottle which are particularly susceptible to weakness due to localized thinning, without over-weighting the bottle.
Embodiments of the present invention will now be described by way of example only with reference to the accompanying drawings, in which:
Figure 1 is a schematic cross-sectional side view, from a first direction, of a preform in accordance with a first embodiment of the present invention, and also showing a front shape of a bottle to be blow-moulded from the preform;
Figure 2 is a schematic cross-sectional side view, from a second direction, of the preform of Figure 1, and also showing a side shape of the bottle shown in Figure 1 ;
Figure 3 is a schematic cross-section on line A-A through the preform of Figure 1 ;
Figure 4 is a schematic cross-section on line B-B through the preform of Figure 1 ; and
Figure 5 is a schematic cross-section on lines C-C and D-D through the preform of Figure 1.
Referring to Figures 1 to 5, there is shown a preform 2, for blow moulding a container 3 such as a bottle, in accordance with an embodiment of the present invention, the preform having been formed by an injection moulding process. The preform 2 comprises a thermoplastic material, such as PET. The elongate preform 2 has a conventional hollow structure and comprises a neck finish 4, which may be threaded, including an annular closure seating flange 6, at an open end 8 of the preform 2, a main body section 10 and a closed end 12 having a convex outer surface 14, and a corresponding concave inner surface 16, which are typically substantially hemispherical. The main body section 10 is substantially cylindrical.
The main body section 10 has an elongate, longitudinally extending inner surface 18 and an elongate, longitudinally extending outer surface 20. The outer surface 20 has a circular cross-section, and typically is substantially right cylindrical.
Optionally, the inner surface 18 has a small taper, of a draft angle typically less than , along the entire length or at least towards the closed end 12 to enable the injection moulded preform 2 readily to be removed from the core of the injection mould. Correspondingly, optionally the outer surface 20 has a small taper, of a draft angle typically less than , along the entire length or at least towards the closed end 12 to enable the injection moulded preform readily to be removed from the moulding block of the injection mould.
The inner surface 18 and outer surface 20 are each centered about a longitudinal axis L-L of the preform 2. The inner and outer surfaces 18, 20 define therebetween a wall 22 of the body section 10.
The wall 22 of the body section 10 has at least one locally thickened portion 24, 26 along the body section 10. Each locally thickened portion 24, 26 is thicker than adjacent first and second thinner portions 28, 30; 32, 34 located at respective opposite longitudinal ends of the thickened portion 24, 26. The thickened portion 24, 26 has an inner surface portion 36, 38 which is nearer to the longitudinal axis L-L than respective first and second inner surface portions 40, 42; 44, 46 of the first and second thinner portions 28, 30; 32, 34.
The wall thickness changes between the locally thickened portion 24, 26 and the adjacent first and second thinner portions 28, 30; 32, 34 are smoothly continuously inclined in the longitudinal direction. The preform 2 comprises first and second inclined inner faces 48, 50; 52, 54, each at a respective first and second blend angle α, β, relative to the longitudinal axis L-L, for the respective first and second inner surface portions 40, 42; 44, 46 extending away from the locally thickened portion 24, 26. The first and second inclined inner faces 48, 50; 52, 54, are respectively oriented towards the open end 8 and the closed end 12, and the first blend angle a is smaller than the second blend angle β.
The locally thickened portion 24, 26 defines a ridge 56, 58 on the inner surface 18. The ridge 56, 58 is linear and extends orthogonally to the longitudinal axis L-L, and along an angular segment 60 of less than 90° of the inner surface 18.
The first and second thinner portions 32, 30 comprises a part of a longitudinally extending thickened element 62 which, along its length, is thicker than laterally adjacent regions 64, 66 of the wall 22 on respective opposite lateral sides of the element 62. The element 62 comprises a radially inwardly directed angular segment. At least a part of the element 62 has a planar chordal inner surface 68.
The preform 2 comprises two locally thickened portions 24, 26, each provided at a respective one of two longitudinally spaced locations along the body section 10. A first locally thickened portion 24 is located at a lowermost third of the length of the body section 10 adjacent to the closed end 12 and a second locally thickened portion 26 is located at an uppermost third of the length of the body section 10 adjacent to the open end 8.
The body section 10 is longitudinally symmetrical and has a plurality of locally thickened portions 24, 26 annularly disposed around the preform 2. The inner surface 18 has an n-fold longitudinal axis of symmetry, where n is at least 2, typically 2 as in the illustrated embodiment, for example 2, 3, 4, 5 or 6, or any larger number. The body section 10 has a plurality of locally thickened portions 24, 26 alternating around the circumference of the preform 2 with wall portions 70 of constant thickness. The portions 70 of constant thickness extend for substantially the entire length of the body section 10. The portions 70 of constant thickness have outer and inner surfaces 18, 20 which extend substantially parallel to the longitudinal axis, optionally with a draft angle of less than 1 ° extending from the closed end 12 to the open end 8.
Along at least one angular segment of the body section 10 there is provided, in a direction from the closed end 12 to the open end 8, a thickening 72 compared to the laterally adjacent regions 64, 66 on respective opposite lateral sides of the thickening 72.
The thickening comprises a first ramp section of increasing wall thickness, for example formed of first thinner portion 28; a second ramp section of decreasing wall thickness, for example formed of second thinner portion 30; an elongate constant thickness section, for example formed of longitudinally extending thickened element 62; a third ramp section of increasing wall thickness, for example formed of first thinner portion 32; and a fourth ramp section of decreasing wall thickness, for example formed of second thinner portion 30.
The first and second ramp sections 28, 30 define a first transverse ridge 56 therebetween which is closer to the longitudinal axis than the first and second ramp sections 28, 30. The third and fourth ramp sections 32, 34 define a second transverse ridge 58 therebetween which is closer to the longitudinal axis than the third and fourth ramp sections 32, 34. The elongate constant thickness section 62 has opposed linear longitudinally extending edges 74, 76. As shown in the illustrated embodiment, a respective thickening 72 is provided along each of two opposed angular segments of the body section. The wall thickness changes provided by the ramp sections are smooth so as to avoid any stress concentrations in the preform 2 or the resultant blow moulded container 3.
Figure 3 is a schematic cross-section on line A-A through the preform 2, and in the illustrated embodiment the constant wall thickness x at that point (Point D) is 2.0 mm. Figure 4 is a schematic cross-section on line B-B through the preform 2, and in the illustrated embodiment the opposed elongate constant thickness sections 62 have a maximum wall thickness y of 2.5 mm, alternating with the constant wall thickness x of 2.0 mm, this structure being at Point D. Figure 5 is a schematic cross-section on lines C- C and D-D through the preform 2, and in the illustrated embodiment the opposed ridges 56. 58 have a maximum wall thickness z of 3.0 mm, alternating with the constant wall thickness x of 2.0 mm, this structure being at Points A and C.
The thickening 72 typically extends for substantially the entire length, parallel to axis L- L, of the main body section 10. However, depending upon the shape and configuration of the desired blow moulded container to be made from the preform 2, the thickening 72
may alternatively extend for only a proportion, even a minor proportion (i.e. less than 50%), of the length of the main body section 10.
In alternative embodiments, the n-fold axis of symmetry for the thickenings 72 may have a different value, for example 3 for making a container having a substantially triangular cross-section, or 8 or greater for making a multi-faceted container.
In the stretch blow moulding step, the preform illustrated in Figures 1 to 5 is heated and inserted into a stretch blow moulding apparatus, and is stretch blow moulded from the substantially tubular shape to the shape desired for the final container 3 As shown in Figures 1 and 2, the present invention has particular application in a method for blow moulding a preform 2 to form a container 3 having a non-circular cross-section including first opposed faces 80, 82 separated by a major internal dimension and second opposed faces 84, 86 separated by a minor internal dimension In such a method, the preform 2 is rotationally oriented in a blow moulding apparatus so that the at least one locally thickened portion 24, 26, or the thickening 72, is oriented towards a moulding surface for moulding such a first opposed face 80, 82.
Points A, B, C and D indicated for the preform 2 correlate to Points A, B, C and D indicated for the container 3 stretch blow-moulded therefrom.
As shown in Figures 1 and 2, the locally thickened portions 24, 26, or thickenings 72, are rotationally oriented so that each lower ridge 56 substantially forms a respective bottom corner 88 of the container 3 which is located between the container base 90 and the respective first opposed faces 80, 82. In the illustrated embodiment, the stretch ratio of the thermoplastic material forming that bottom corner 88 is higher than for any other portion of the container 3, and so the thickened preform material at the ridge 56 prevents over-thinning at that corner 88. Similarly, each upper ridge 58 substantially forms a respective upper corner 92 of the container 3 which is located between the container shoulder 94 and the respective first opposed faces 80, 82. The first opposed faces 80, 82 are substantially formed from the central portion of the thickening 72 between the ridges 56, 58, in particular the second ramp section formed of second thinner portion 30;
the elongate constant thickness section formed of longitudinally extending thickened element 62; and the third ramp section formed of first thinner portion 32.
The relatively thickened wall portions of the preform 2 may be preferentially stretched, by having a higher radial stretch ratio, as compared to the relatively thinned wall portions, to provide a substantially uniform sidewall thickness in the resultant non- circular container 3. Even in highly stretched regions of the sidewall, the desired minimum wall thickness has been maintained because these regions are formed from the relatively thickened wall portions of the preform 2.
The shaping of the preform according to the invention may be regarded as an "ovalisation" of the preform where there are vertical areas on the inner surface that are thickened to help maintain wall thickness in the highly stretched areas of the bottle. These thickened areas may be considered to constitute a plurality of integral longitudinal thickened ribs disposed in a mutually spaced configuration around the circular inner surface. Typically this means two sides of a preform being thicker than the other two sides as shown in Figures 1 and 2. Such an "ovalisation" structure is achieved by undercutting the core, which minimizes excess material while providing additional material precisely where it is required in the container and particularly at highly stretched corners of container faces remote from the longitudinal axis.
The invention also provides an injection mould or an extrusion compression mould for forming a preform according to the present invention. The injection mould comprises a central elongate core and a mould block defining a cavity for receiving the core. The central elongate core has an outer surface corresponding to the inner surface of the preform. The core includes a convex elongate, longitudinally extending first moulding surface for moulding an internal surface of a body section of the preform, the first moulding surface having a cross-section centered about a longitudinal axis. The cavity includes a concave elongate, longitudinally extending second moulding surface for moulding an external surface of the body section of the preform, the second moulding surface having a circular cross-section centered about the longitudinal axis. In this way, the mould can readily injection mould the preform.
In particular, the elongate core may be of an injection mould or an extrusion compression mould for forming a moulded preform of a thermoplastic material for stretch blow moulding to form a container. The core comprises a fixed end, an elongate body and free end, the elongate body defining a convex elongate, longitudinally extending moulding surface for moulding an internal surface of a body section of the preform, the first moulding surface having a cross-section centered about a longitudinal axis, and being substantially cylindrical with an acute draft angle to provide that the free end has a smaller diameter than that of the fixed end, the moulding surface including at least one concave undercut where the core is machined below the draft angle of the core
The present invention also provides a method for blow moulding a preform according to the present invention, to form a container. In particular, the container has a non-circular cross-section including first opposed faces separated by a major internal dimension and second opposed faces separated by a minor internal dimension. The method includes the step of rotationally orienting the preform in a blow moulding apparatus so that the at least one locally thickened portion is oriented towards moulding surface for moulding a first opposed face.
Although various embodiments of the invention have been described in detail, it will be apparent to those skilled in the art that other modifications of the apparatus and methods may be employed that are within the scope of the invention as defined in the appended claims.
Claims
1. A preform for blow moulding to form a container, the preform being formed of a thermoplastic material, the preform comprising a neck finish at an open end of the preform, an elongate body section and a closed end, wherein the body section has elongate, longitudinally extending inner and outer surfaces each centered about a longitudinal axis of the preform, the inner and outer surfaces defining therebetween a wall of the body section, wherein the wall of the body section has at least one locally thickened portion along the body section, the locally thickened portion being thicker than adjacent first and second thinner portions at respective opposite longitudinal ends of the thickened portion, the thickened portion having an inner surface portion which is nearer to the longitudinal axis than respective first and second inner surface portions of the first and second thinner portions.
2. A preform according to claim 1 wherein the wall thickness changes between the locally thickened portion and the adjacent first and second thinner portions are smoothly continuously inclined in the longitudinal direction.
3. A preform according to claim 2 comprising first and second inclined inner faces, each at a respective first and second blend angle, relative to the longitudinal axis, for the respective first and second inner surface portions extending away from the locally thickened portion.
4. A preform according to claim 3 wherein the first and second inclined inner faces are respectively oriented towards the open end and the closed end, and the first blend angle is smaller than the second blend angle.
5. A preform according to any foregoing claim wherein the locally thickened portion defines a ridge on the inner surface.
6. A preform according to claim 5 wherein the ridge is linear and extends orthogonally to the longitudinal axis.
7. A preform according to claim 6 wherein the ridge extends along an angular segment of less than 90° of the inner surface.
8. A preform according to any foregoing claim wherein at least one of the first and second thinner portions comprises a part of a longitudinally extending thickened element which, along its length, is thicker than laterally adjacent regions of the wall on respective opposite lateral sides of the element.
9. A preform according to claim 8 wherein the element comprises a radially inwardly directed angular segment.
10. A preform according to claim 8 or claim 9 wherein at least a part of the longitudinally extending thickened element has a planar chordal inner surface.
1 1. A preform according to any foregoing claim comprising two locally thickened portions, each provided at a respective one of two longitudinally spaced locations along the body section.
12. A preform according to claim 11 wherein a first locally thickened portion is located at a lowermost third of the length of the body section adjacent to the closed end and a second locally thickened portion is located at an uppermost third of the length of the body section adjacent to the open end.
13. A preform according to any foregoing claim wherein the body section is longitudinally symmetrical and has a plurality of locally thickened portions annularly disposed around the preform.
14. A preform according to any foregoing claim wherein the elongate, longitudinally extending inner surface has an n-fold longitudinal axis of symmetry, where n is at least 2.
15. A preform according to claim 14 wherein n is 2, 3, 4, 5 or 6, or any larger number.
16. A preform according to any foregoing claim wherein the body section has a plurality of locally thickened portions alternating around the circumference of the preform with portions of constant thickness.
17. A preform according to claim 16 wherein the portions of constant thickness extend for substantially the entire length of the body section.
18. A preform according to claim 17 wherein the portions of constant thickness have outer and inner surfaces which extend substantially parallel to the longitudinal axis, optionally with a draft angle of less than 1 ° extending from the closed end to the open end.
19. A preform according to claim 1 wherein along at least one angular segment of the body section there is provided, in a direction from the open end to the closed end, a thickening compared to laterally adjacent regions on respective opposite lateral sides of the thickening, the thickening comprising a first ramp section of increasing wall thickness, a second ramp section of decreasing wall thickness, an elongate constant thickness section, a third ramp section of increasing wall thickness and a fourth ramp section of decreasing wall thickness.
20. A preform according to claim 19 wherein the first and second ramp sections define a first transverse ridge therebetween which is closer to the longitudinal axis than the first and second ramp sections.
21. A preform according to claim 19 or claim 20 wherein the third and fourth ramp sections define a second transverse ridge therebetween which is closer to the longitudinal axis than the third and fourth ramp sections.
22. A preform according to any one of claims 19 to 21 wherein the elongate constant thickness section has opposed linear longitudinally extending edges.
23. A preform according to any one of claims 19 to 22 wherein a respective thickening is provided along each of two opposed angular segments of the body section.
24. A preform according to any foregoing claim wherein the elongate, longitudinally extending outer surface has a circular cross-section.
25. A preform according to claim 24 wherein the elongate, longitudinally extending outer surface is substantially right cylindrical, optionally with a draft angle of less than 1 ° extending from the closed end to the open end.
26. A mould part for forming a preform according to any foregoing claim, the mould part comprising a central elongate core having an outer surface corresponding to the inner surface of the preform.
27. A mould part according to claim 26 which is adapted for use in an injection mould or an extrusion compression mould.
28. An elongate core of an injection mould or an extrusion compression mould for forming a moulded preform of a thermoplastic material for stretch blow moulding to form a container, the core comprising a fixed end, an elongate body and a free end, the elongate body defining a convex elongate, longitudinally extending moulding surface for moulding an internal surface of a body section of the preform, the first moulding surface having a cross-section centered about a longitudinal axis, and being substantially cylindrical with an acute draft angle to provide that the free end has a smaller diameter than that of the fixed end, the moulding surface including at least one concave undercut where the core is machined below the draft angle of the core.
29. A method for stretch blow moulding a preform according to any one of claims 1 to 25 to form a container having a non-circular cross-section including first opposed faces separated by a major internal dimension and second opposed faces separated by a minor internal dimension, said method including the step of:
a. rotationally orienting the preform in a blow moulding apparatus so that the at least one locally thickened portion is oriented towards moulding surface for moulding a first opposed face.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11808196.7A EP2655030B1 (en) | 2010-12-20 | 2011-12-20 | Preform for blow moulding a container and method for stretch blow moulding the preform into containers of non-circular cross section |
US13/996,316 US9694531B2 (en) | 2010-12-20 | 2011-12-20 | Preforms for blow moulding |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1021529.1A GB2486647B (en) | 2010-12-20 | 2010-12-20 | Preforms for blow moulding |
GB1021529.1 | 2010-12-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2012084995A1 true WO2012084995A1 (en) | 2012-06-28 |
Family
ID=43598630
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2011/073467 WO2012084995A1 (en) | 2010-12-20 | 2011-12-20 | Preform for blow moulding a container, mould part and elongate core for moulding the preform and method for stretch blow moulding the preform |
Country Status (4)
Country | Link |
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US (1) | US9694531B2 (en) |
EP (1) | EP2655030B1 (en) |
GB (1) | GB2486647B (en) |
WO (1) | WO2012084995A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9849620B2 (en) | 2014-03-21 | 2017-12-26 | Husky Injection Molding Systems Ltd. | Container preform |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH707196A1 (en) * | 2012-11-07 | 2014-05-15 | Alpla Werke | An injection molded preform for the production of plastic containers in a stretch blow molding. |
WO2019104394A1 (en) * | 2017-11-30 | 2019-06-06 | Integrated Plastics Pty Limited | Preforms for stretch-blow-moulding containers and continuous blow moulding machine producing the containers |
US20220024082A1 (en) * | 2021-07-08 | 2022-01-27 | Schock Gmbh | Casting in the form of a sink |
DE102021125486A1 (en) * | 2021-10-01 | 2023-04-06 | Optipack Gmbh | Process for making a preform and preform |
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- 2011-12-20 WO PCT/EP2011/073467 patent/WO2012084995A1/en active Application Filing
- 2011-12-20 EP EP11808196.7A patent/EP2655030B1/en not_active Not-in-force
- 2011-12-20 US US13/996,316 patent/US9694531B2/en not_active Expired - Fee Related
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JP2002240136A (en) * | 2001-02-20 | 2002-08-28 | Kanamori Tobei Shoji Kk | Preform for heat-resistant pet bottle |
DE10234037A1 (en) * | 2002-07-26 | 2004-02-12 | Bekum Maschinenfabriken Gmbh | Plastic preform for production of non-round, particularly oval, containers has variable wall thickness around the circumference to compensate for different degrees of stretch |
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Also Published As
Publication number | Publication date |
---|---|
US20140295119A1 (en) | 2014-10-02 |
GB2486647B (en) | 2013-06-19 |
GB2486647A (en) | 2012-06-27 |
US9694531B2 (en) | 2017-07-04 |
EP2655030A1 (en) | 2013-10-30 |
GB201021529D0 (en) | 2011-02-02 |
EP2655030B1 (en) | 2016-11-02 |
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